TM 1-1520-238-10
7A-57
M01-273
170
160
150
100
130
120
140
90
30
70
80
50
60
40
20
180
170
110
150
140
160
120
40
130
80
90
0
70
100
60
50
30
20
10
180
20
150
40
50
90
60
80
1400
1000
800
800
1000
1200
1200
600
70
TOTAL FUEL FLOW – LB/HOUR
160
600
170
140
100
120
110
130
PRESSURE ALTITUDE - 14,000 FEET
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
TOTAL FUEL FLOW – LB/HOUR
CRUISE
110
30
30
100
50
60
40
80
90
70
30
100
50
60
40
80
90
70
10
D
F = 10.0 SQ FT
D
Q – %
0
20
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
MAX END
OR
MAX R/C
FAT=–40C
FAT=–50C
AH–64A
CRUISE
T700–GE–701C
AIRSPEED
INDICATED
KNOTS
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
VNE
VNE
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-16.
Cruise Chart, 14,000 Feet, –50 C and –40 C (Sheet 1 of 5)
